WEKO3
アイテム
{"_buckets": {"deposit": "e41b8e05-77c1-472f-a505-f97e16811f67"}, "_deposit": {"created_by": 1, "id": "45284", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "45284"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00045284", "sets": ["1893", "1917"]}, "author_link": ["473875", "473874", "473871", "473872", "473873", "473876"], "item_3_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "風上差分法による鈍頭物体まわりの超音速流れの解析"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1989-07", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "12", "bibliographicVolumeNumber": "1025", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-1025", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A numerical calculation of hypersonic flow around two-dimensional blunt bodies is presented. The Euler equations in conservation form are calculated by the first order accurate Osher upwind scheme. In this calculation, two types of boundary conditions on the body surface are tested. One is the conventional condition for Euler equations, and ther other is a new form in which flux is conserved throughout the whole flow field. Results show that the conventional boundary conditions do not provide reasonable solutions at high Mach numbers (M \u003e 2.4), while the new boundary conditions do. The calculation is stably executed, and the shock is clearly captured from low to high Mach numbers.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR1025000", "subitem_description_type": "Other"}]}, "item_3_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: NAL TR-1025", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory(NAL)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0389-4010", "subitem_source_identifier_type": "ISSN"}]}, "item_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: NAL-MATCH"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 航空宇宙技術研究所"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_3_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 9"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "航空宇宙技術研究所数理解析部"}, {"subitem_text_value": "航空宇宙技術研究所数理解析部"}, {"subitem_text_value": "東京農工大学"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Computational Sciences Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Computational Sciences Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo University of Agriculture and Technology"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "和田, 安弘"}], "nameIdentifiers": [{"nameIdentifier": "473871", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小川, 哲"}], "nameIdentifiers": [{"nameIdentifier": "473872", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "新井, 紀夫"}], "nameIdentifiers": [{"nameIdentifier": "473873", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "WADA, Yasuhiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473874", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "OGAWA, Satoru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473875", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "ARAI, Norio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473876", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-29"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "naltr01025.pdf", "filesize": [{"value": "732.5 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 732500.0, "url": {"label": "naltr01025.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/45284/files/naltr01025.pdf"}, "version_id": "30d704a1-5437-4215-93ca-6f73421651a4"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "item_resource_type": {"attribute_name": "資源タイプ", "attribute_value_mlt": [{"resourcetype": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "A Numerical Calculation of Hypersonic Flow Around Blunt Bodies Using Upwind Difference Scheme", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "A Numerical Calculation of Hypersonic Flow Around Blunt Bodies Using Upwind Difference Scheme", "subitem_title_language": "en"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/45284", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "45284", "relation": {}, "relation_version_is_last": true, "title": ["A Numerical Calculation of Hypersonic Flow Around Blunt Bodies Using Upwind Difference Scheme"], "weko_shared_id": -1}
A Numerical Calculation of Hypersonic Flow Around Blunt Bodies Using Upwind Difference Scheme
https://jaxa.repo.nii.ac.jp/records/45284
https://jaxa.repo.nii.ac.jp/records/452843bec1eed-3786-4543-9f6d-d22033f0f47f
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr01025.pdf (732.5 kB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A Numerical Calculation of Hypersonic Flow Around Blunt Bodies Using Upwind Difference Scheme | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | 風上差分法による鈍頭物体まわりの超音速流れの解析 | |||||
著者 |
和田, 安弘
× 和田, 安弘× 小川, 哲× 新井, 紀夫× WADA, Yasuhiro× OGAWA, Satoru× ARAI, Norio |
|||||
著者所属 | ||||||
航空宇宙技術研究所数理解析部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所数理解析部 | ||||||
著者所属 | ||||||
東京農工大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Computational Sciences Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Computational Sciences Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Agriculture and Technology | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-1025 巻 1025, p. 12, 発行日 1989-07 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A numerical calculation of hypersonic flow around two-dimensional blunt bodies is presented. The Euler equations in conservation form are calculated by the first order accurate Osher upwind scheme. In this calculation, two types of boundary conditions on the body surface are tested. One is the conventional condition for Euler equations, and ther other is a new form in which flux is conserved throughout the whole flow field. Results show that the conventional boundary conditions do not provide reasonable solutions at high Mach numbers (M > 2.4), while the new boundary conditions do. The calculation is stably executed, and the shock is clearly captured from low to high Mach numbers. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR1025000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1025 |